JP2004520209A5 - - Google Patents

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Publication number
JP2004520209A5
JP2004520209A5 JP2001518316A JP2001518316A JP2004520209A5 JP 2004520209 A5 JP2004520209 A5 JP 2004520209A5 JP 2001518316 A JP2001518316 A JP 2001518316A JP 2001518316 A JP2001518316 A JP 2001518316A JP 2004520209 A5 JP2004520209 A5 JP 2004520209A5
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JP
Japan
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2001518316A
Other languages
Japanese (ja)
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JP2004520209A (ja
JP3998978B2 (ja
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Publication date
Priority claimed from GBGB9919787.3A external-priority patent/GB9919787D0/en
Application filed filed Critical
Publication of JP2004520209A publication Critical patent/JP2004520209A/ja
Publication of JP2004520209A5 publication Critical patent/JP2004520209A5/ja
Application granted granted Critical
Publication of JP3998978B2 publication Critical patent/JP3998978B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001518316A 1999-08-21 2000-08-16 構造物の製造とアッセンブリィ Expired - Fee Related JP3998978B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9919787.3A GB9919787D0 (en) 1999-08-21 1999-08-21 Manufacture and assembly of structures
PCT/GB2000/003165 WO2001014208A1 (en) 1999-08-21 2000-08-16 Manufacture and assembly of structures

Publications (3)

Publication Number Publication Date
JP2004520209A JP2004520209A (ja) 2004-07-08
JP2004520209A5 true JP2004520209A5 (enrdf_load_stackoverflow) 2007-03-22
JP3998978B2 JP3998978B2 (ja) 2007-10-31

Family

ID=10859545

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001518316A Expired - Fee Related JP3998978B2 (ja) 1999-08-21 2000-08-16 構造物の製造とアッセンブリィ

Country Status (9)

Country Link
US (1) US6907651B1 (enrdf_load_stackoverflow)
EP (1) EP1204550B1 (enrdf_load_stackoverflow)
JP (1) JP3998978B2 (enrdf_load_stackoverflow)
AT (1) ATE241498T1 (enrdf_load_stackoverflow)
AU (1) AU6584900A (enrdf_load_stackoverflow)
DE (1) DE60003043T2 (enrdf_load_stackoverflow)
ES (1) ES2200909T3 (enrdf_load_stackoverflow)
GB (1) GB9919787D0 (enrdf_load_stackoverflow)
WO (1) WO2001014208A1 (enrdf_load_stackoverflow)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0126957D0 (en) * 2001-11-09 2002-01-02 Bae Systems Plc Manufacture and assembly of structures
GB0222288D0 (en) * 2002-09-25 2002-10-30 Airbus Uk Ltd Method and apparatus for joining aircraft components
US7487901B2 (en) * 2004-07-29 2009-02-10 The Boeing Company Friction stir welding of joints with shims
GB0519364D0 (en) 2005-09-22 2005-11-02 Airbus Uk Ltd Assembly of aircraft components
GB0525690D0 (en) * 2005-12-16 2006-01-25 Airbus Uk Ltd Assembly of aircraft components
FR2905739B1 (fr) * 2006-09-08 2008-11-07 Airbus France Sas Assemblage de panneaux et procede de montage d'un assemblage de panneaux
JP4657194B2 (ja) * 2006-11-20 2011-03-23 本田技研工業株式会社 前縁スキンの段差調整構造および前縁スキンの組付方法
US20090040247A1 (en) * 2007-08-07 2009-02-12 Mark Cato Micro shim for moving coil actuator
GB0720702D0 (en) * 2007-10-23 2007-12-05 Airbus Uk Ltd A shim for arrangement against a structural component and a method making a shim
US9731418B2 (en) 2008-01-25 2017-08-15 Systems Machine Automation Components Corporation Methods and apparatus for closed loop force control in a linear actuator
US9381649B2 (en) 2012-06-25 2016-07-05 Systems Machine Automation Components Corporation Robotic finger
DE102008010197B4 (de) 2008-02-20 2012-03-22 Airbus Operations Gmbh Verfahren zum Verbinden von zwei Rumpfsektionen unter Schaffung eines Querstoßes sowie Querstoßverbindung
US9586367B2 (en) * 2008-11-04 2017-03-07 Lockheed Martin Corporation Composite laminate thickness compensation
EP2487106B1 (en) * 2009-10-08 2018-07-25 Mitsubishi Heavy Industries, Ltd. Composite material structure, as well as aircraft wing and fuselage provided therewith
US9186849B2 (en) * 2009-12-10 2015-11-17 Michael Spellman Composite part manufacturing compensation system and method
US9780634B2 (en) 2010-09-23 2017-10-03 Systems Machine Automation Components Corporation Low cost multi-coil linear actuator configured to accommodate a variable number of coils
ES2396881B1 (es) * 2010-11-30 2014-01-29 Airbus Operations, S.L. Disposición de interfaz entre dos componentes de una estructura de una aeronave usando una pieza de sellado.
WO2014004589A1 (en) 2012-06-25 2014-01-03 Neff Edward A Low-cost, reduced diameter linear actuator
US10807248B2 (en) 2014-01-31 2020-10-20 Systems, Machines, Automation Components Corporation Direct drive brushless motor for robotic finger
US9871435B2 (en) 2014-01-31 2018-01-16 Systems, Machines, Automation Components Corporation Direct drive motor for robotic finger
US10429211B2 (en) 2015-07-10 2019-10-01 Systems, Machines, Automation Components Corporation Apparatus and methods for linear actuator with piston assembly having an integrated controller and encoder
EP3353558A1 (en) 2015-09-24 2018-08-01 Systems, Machines, Automation Components Corporation Magnetically-latched actuator
US10675723B1 (en) 2016-04-08 2020-06-09 Systems, Machines, Automation Components Corporation Methods and apparatus for inserting a threaded fastener using a linear rotary actuator
US10865085B1 (en) 2016-04-08 2020-12-15 Systems, Machines, Automation Components Corporation Methods and apparatus for applying a threaded cap using a linear rotary actuator
US10205355B2 (en) 2017-01-03 2019-02-12 Systems, Machines, Automation Components Corporation High-torque, low-current brushless motor
DE102017222897A1 (de) * 2017-12-15 2019-06-19 MTU Aero Engines AG Faserverbund-Bauteilanordnung, Faserverbund-Bauteilsystem und Verfahren zum Herstellen eines Faserverbund-Bauteilsystems
CN115648636B (zh) * 2022-09-28 2024-11-12 成都飞机工业(集团)有限责任公司 复合材料制件胶接方法、装置、存储介质及设备

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3609116A (en) 1968-12-06 1971-09-28 Gen Dynamics Corp Moldable shim material for dimensional and aerodynamic surface control of aerospace structure
US4478915A (en) 1983-11-07 1984-10-23 United Technologies Corporation Corrosion resistant shim for electrically joining incompatible materials
US4861643A (en) 1987-03-13 1989-08-29 The Boeing Company Aerospace structure having a cast-in-place noncompressible void filler
US5385050A (en) 1992-04-07 1995-01-31 Northrop Grumman Corporation Gap measurement for shim manufacture

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